A satellite is revolving round the earth with orbital speed v0. If it stops suddenly, the speed with which it will strike the surface of earth would be
(ve= escape velocity of a particle on earth's surface)
Let r be the radius of the satellite.Then
v20=GMr ------------------(1)
R = radius of earth.
Applying conservation of mechanical energy between points A and B, we have:
12mv2=−GMmr−(−GMmR)
or v2=2GMR−2GMr
= v2e−2v20
or v=√v2e−2v20